[fltsim.0] title=Angel sim=Angel model= panel= sound= texture= kb_checklists= ui_manufacturer=Robbins Shipyard ui_type=Boat "Angel" ui_variation=Harbor Tours atc_heavy=0 atc_airline= [General] atc_type= atc_model= editable=0 performance=Max Speed\t35 kts\nCruise Speed\t30 kts\nMaximum Range\t624 nm\nFuel Capacity\t60 gals\n MPG 8\nMax Gross Weight\t12500lbs\nSeating\t\t50\nUseful Load\15000lbs\n Category=airplane [Reference Speeds] flaps_up_stall_speed = 040 full_flaps_stall_speed = 000 cruise_speed = 030 max_indicated_speed = 035 max_mach = 0.10 [WEIGHT_AND_BALANCE] max_gross_weight = 125000 empty_weight = 110000 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0,0,0 ;ZXY distance from specified datum max_number_of_stations = 30 station_load.0 = 500, 0,0,0 ;Fuel station_load.1 = 10000, 0,0,0 ;Passengers station_load.2 = 1000, 0,0,0; Fresh Water station_load.3 = 1000, 0,0,0; Luggage, misc. station_load.4 = 500, 0,0,0; Supplies ;Moments of Inertia empty_weight_pitch_MOI = 16304110 empty_weight_roll_MOI = 1152310 empty_weight_yaw_MOI = 1900000 empty_weight_coupled_MOI = 0 [contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float ; 0 Class (0=floats) ; 1 Longitudinal Position (feet) ; 2 Lateral Position (feet) ; 3 Vertical Position (feet) ; 4 Impact Damage Threshold (Feet Per Minute) ; 5 Brake Map (0=None, 1=Left, 2=Right) [N/A] ; 6 Wheel Radius (feet) ; 7 Steer Angle (degrees) ; 8 Static Compression (feet) (0=rigid) ; 9 Max/Static Compression Ratio ;10 Damping Ratio/Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) ;11 Extension Time (seconds) ;12 Retraction Time (seconds) ;13 Sound Type ;14 Airspeed limit for retraction (KIAS) ;15 Airspeed that gear gets damage at (KIAS) ; 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 ; 0 Z X Y FPM BM WR SA SC Max DR ET RT SND RL GD point.0=1, 50.6, 0, -6.70, 1181, 0, 0.596, 0.0, 0.0, 2.5, 0.9516, 4.8, 4.8, 2, 184.0, 184.0 point.1=1, 50.6, 0, -6.70, 1181, 0, 0.596, 0.0, 0.0, 2.5, 0.9516, 4.8, 4.8, 2, 184.0, 184.0 ;Floats point.2=4, 40,-2.5, -3, 9999, 1, 1, 20, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.3=4, 40, 2.5, -3, 9999, 2, 1, 20, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.4=4, -20,-2.5, -3, 9999, 1, 1, 20, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.5=4, -20, 2.5, -3, 9999, 2, 1, 20, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 ;Set One point.6=4, 40,-9.5, -3, 9999, 1, 1, 20, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.7=4, 40, 9.5, -3, 9999, 2, 1, 20, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 point.8=4, -30,-2.5, -3, 9999, 1, 1, 20, 0.9, 15.5, 0.65, 00, 00, 2, 00, 00 point.9=4, -30, 2.5, -3, 9999, 2, 1, 20, 0.9, 15.5, 0.65, 00, 00, 3, 00, 00 ;Set Two static_pitch = 1 static_cg_height = 4.0 gear_system_type = 1 [Views] ;ZXY distance from reference datum (feet) eyepoint= 26.20, -6.5, 17.60 //(feet) longitudinal, lateral, vertical distance from reference datum [EFFECTS] wake=fx_wake_l water=fx_spray [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 30, -8, 18, fx_vclight, light.1 = 4, 30, -5, 18, fx_vclight, light.2 = 3, 51, -.8, 9.3, fx_navgreh, light.3 = 3, 51, .6, 9.3, fx_navredh, [flight_tuning] cruise_lift_scalar = .000 parasite_drag_scalar = 1.000 induced_drag_scalar = 1.000 elevator_effectiveness = .000 aileron_effectiveness = 000 rudder_effectiveness = 1.5 pitch_stability = .01000 roll_stability = .01000 yaw_stability = 1.000 elevator_trim_effectiveness = .000 aileron_trim_effectiveness = .000 rudder_trim_effectiveness = 1.500 [airplane_geometry] wing_area = 825.0 ;Square feet wing_span = 211.4 wing_root_chord = 48.8 wing_dihedral = 7.0 ;Degrees wing_incidence = 2.0 ;Degrees wing_twist = -1.0 ;Degrees oswald_efficiency_factor = 0.68 ;Measure of lift effeciency of wing wing_winglets_flag = 1 ;Are winglets available? wing_sweep = 37.5 ;Degrees, wing leading edge wing_pos_apex_lon = -68.2 ;Z distance from ref point wing_pos_apex_vert = 0 ;Y distance from ref point htail_area = 1470 ;Square feet htail_span = 72.8 htail_pos_lon = -210.0 ;Z distance from ref point htail_pos_vert = 0.0 ;Y distance from ref point htail_incidence = 0.0 ;Degrees htail_sweep = 37.5 ;horizontal tail leading edge vtail_area = 1060 ;Square feet vtail_span = 37.1 ;tip to body vtail_sweep = 45.0 ;Degrees, vertical tail leading edge vtail_pos_lon = -198.5 ;Z distance from ref point vtail_pos_vert = 26.1 ;Y from ref point elevator_area = 0 ;Square feet aileron_area = 0 ;Square feet rudder_area = 200 ;Square feet elevator_up_limit = 0 ;Degrees elevator_down_limit = 0 ;Degrees aileron_up_limit = 0 ;Degrees aileron_down_limit = 0 ;Degrees rudder_limit = 31.5 ;Degrees elevator_trim_limit = 0 ;Degrees spoiler_limit = 0 ;Degrees spoilerons_available = 0 ;Spoilerons Available? aileron_to_spoileron_gain = 0 ;Aileron to spoileron gain min_ailerons_for_spoilerons = 0 ;Degrees min_flaps_for_spoilerons = 0 ;Minimum flap handle position when spoilerons activate auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 ;[flaps.0] ;type = 0 [fuel] LeftMain = -8.46, -6.45, 0.0, 30.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -8.46, 6.45, 0.0, 30.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [electrical] electric_always_available = 1 [Radios] // Radio Type = available, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 1 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [gear_warning_system] gear_warning_available = 0 [GeneralEngineData] engine_type = 1 ;1=Jet Engine.0 = -4,0,0 ;ZXY distance from ref datum Engine.1 = 4,0,0 fuel_flow_scalar = .001 ;Scalar for fuel flow efficiency min_throttle_limit = -.15 ;neg for turbine reverser [TurbineEngineData] fuel_flow_gain = 0.05 ;Gain on fuel flow inlet_area = 2.0 ;Square Feet, engine nacelle inlet area rated_N2_rpm = 3600 ;RPM, 2nd stage compressor rated value static_thrust = 20000 ;Lbs, max rated static thrust at SL afterburner_available = 0 ;Afterburner available? reverser_available = 1 ;Thrust reverser available? [jet_engine] thrust_scalar = 1.0 [brakes] parking_brake = 1 ;Parking brake available (Anchor) toe_brakes_scale = 5 ;Brake scalar [hydraulic_system] normal_pressure = 3000 ;PSI electric_pumps = 1 ;electric pumps engine_map = 2,0,0,0 ;pumps [pitot_static] vertical_speed_time_constant = 1 pitot_heat=1.000000 ;Increasing this value will cause a more instantaneous reaction in the VSI [direction_indicators] direction_indicator.0 = 3,0 ;3=Electro-Mag Slaved Compass, 0=NA [attitude_indicators] attitude_indicator.0 = 0 ;0=None [turn_indicators] turn_indicator.0 = 1,0 ;1=Electric Gyro [stall_warning] type = 0 stick_shaker=0 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed=1800.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [keyboard_response] ;Breakpoint speeds (knots) on the keyboard increments of control surfaces. ;Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] ;revised to eliminate bumps gear_bump_nose_magnitude = 3000 ;0 - 10000 gear_bump_nose_direction = 18000 ;0 - 35999 degrees gear_bump_nose_duration = 250000 ;in microseconds gear_bump_left_magnitude = 2700 ;0 - 10000 gear_bump_left_direction = 35500 ;0 - 35999 degrees gear_bump_left_duration = 250000 ;in microseconds gear_bump_right_magnitude = 2700 ;0 - 10000 gear_bump_right_direction = 00500 ;0 - 35999 degrees gear_bump_right_duration = 250000 ;in microseconds ground_bumps_magnitude1 = 1300 ;0 - 10000 ground_bumps_angle1 = 08900 ;0 - 35999 degrees ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ;0 - 10000 ground_bumps_angle2 = 09100 ;0 - 35999 degrees ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 ;0 - 10000 crash_direction1 = 01000 ;0 - 35999 degrees crash_magnitude2 = 10000 ;0 - 10000 crash_direction2 = 9000 ;0 - 35999 degrees crash_period2 = 75000 ;in microseconds crash_duration2 = 2500000 ;in microseconds [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=1 [propeller] propeller_type=1 propeller_diameter=6.883000 propeller_blades=3 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available = 1 minimum_on_ground_beta=1.000000 minimum_reverse_beta=1.000000